A high speed wind tunnel test evaluation of STOL dedicated advanced exhaust nozzle concepts
19th Joint Propulsion Conference ; 1983 ; Seattle , WA , U.S.A.
01.01.1983
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Exhaust nozzle concepts for STOL tactical aircraft
AIAA | 1983
|Test section for a V/STOL wind tunnel
AIAA | 1970
|